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Which outcome occurs when jet engine combustion instabilities trigger acoustic resonance?

A)Increased turbulent kinetic energy
B)Decreased nozzle exit velocity
C)Enhanced laminar flow stability
D)Reduced compressor stall margin

💡 Explanation

Increased turbulent kinetic energy results, because the acoustic resonance amplifies small perturbations driving the flow towards instability by Reynolds stresses, therefore a turbulent flame develops, rather than a stable combustion process alone.

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